• Journal of Electrochemical Science and Technology
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• 제13권1호
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• pp.1-18
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• 2022

Persistent organic pollutants (POPs) and emerging pollutants (EP) are characterized by their difficulty to be removed through biological oxidation processes (BOPs); they persist in the environment and could have adverse effects on the aquatic ecosystem and human health. The electro-oxidation (EO) process has been successfully used as an alternative technique to oxidize many kinds of the aforementioned pollutants in wastewater. However, the EO process has been criticized for its high energy consumption cost and its potential generation of by-products. In order to decrease these drawbacks, its combination with biological oxidation processes has been reported as a solution to reduce costs and to reach high rates of recalcitrant pollutants removal from wastewaters. Thus, the location of EO in the treatment line is an important decision to make, since this decision affects the formation of by-products and biodegradability enhancement. This paper reviews the advantages and disadvantages of EO as a pre and post-treatment in combination with BOPs. A perspective of the EO scale-up is also presented, where hydrodynamics and the relationship of A/V (area of the electrode/working volume of the electrochemical cell) experiments are examined and discussed.

• 한국군사과학기술학회지
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• 제20권6호
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• pp.743-751
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• 2017

To evaluate the structural integrity of the helicopter radome, we performed bird strike analysis using SPH (Smoothed Particle Hydrodynamics) technique. Since the SPH method is a meshfree method, there is no phenomenon such as mesh tangling and it is suitable to predict the dispersion behavior of debris and debris cloud generated by high-speed impact. In order to observe the scattering direction of fractured bolts, the analysis were performed under the condition that the fracture occurs at the proof load. As a result of bird strike analysis, there is no secondary damage as well as the damage due to, the dispersion behavior of the bird model, and the scattering of the fractured bolts and radome. From the additional analysis that were performed to determine the actual bolt fracture, only plastic deformation is predicted since the maximum stress of the bolt does not exceed the ultimate stress.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2010년 춘계학술대회논문집
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• pp.103-108
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• 2010

This article presents computational fluid dynamics (CFD) simulations of nanoparticle movements and flow characteristics in laboratory-scale electrostatic precipitator (ESP) without corona discharge, and for simulation, it uses the commercial CFD program(CFD-ACE) including electrostatic theory and Lagrangian-based equation for nanoparticle movement. For validation of CFD results, a simple cylindrical type of ESP is simulated and numerical prediction shows fairly good agreement with the analytical solution. In particular, the present study investigates the effect of particle diameter, inlet flow rate, and applied electric potential on particle collection efficiency and compares the numerical prediction with the experimental data, showing good agreement. It is found that the particle collection efficiency decreases with increasing inlet flow rate because the particle detention time becomes shorter, whereas it decreases with the increase in nanoparticle diameter and with the decrease of applied electric voltage resulting from smaller terminal electrostatic velocity.

• 동력기계공학회지
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• 제21권3호
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• pp.51-59
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• 2017

In the early design stage of underwater vehicles, it is important to estimate the vehicle's underwater motion performance. The key design elements for the motion are propellers, battery power, and underwater resistance of the vehicle. Small thrusters with motor and propeller are usually used for the UUV(unmanned underwater vehicles). In this study, a multiphysics thruster model combining electro-mechanical and hydrodynamics characteristics was proposed to estimate the thruster performance. To show the applicability of the mathematical model, an sample thruster was used for the derive the unknown parameters of thruster. Hydrodynamic parameters were calculated for a 3D geometry model of the propeller by ANSYS/CFX program. Finally, Matlab/simulink program was used for the numerical simulation to predict the thruster performance from the given voltage/current input to the motor. Also, proved validity of simulation model by experiment test. Test were done by 2 mode(middle/high speed, reverse). The thruster performance curves obtained from this simulation were confirmed to be similar with experiment results.

• 항공우주시스템공학회지
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• 제12권6호
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• pp.1-8
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• 2018

투명 전극에 사용되는 필름인 이방성전도필름은 전도성 입자를 재료로 하여 열 압착법으로 제조되고 있다. 하지만 열 압착법은 낭비되는 재료가 많고 공정이 복잡하다는 단점을 가지고 있으며, 이와 같은 단점을 극복하기 위해 전도성 입자 잉크를 이용한 잉크젯 프린팅 기술을 제안하였다. 잉크의 특성 및 프린팅 조건은 패터닝 선 두께에 영향을 주게 되며, 미세 패터닝을 위한 최적 조건 도출이 중요하다. 본 논문에서는 전도성 입자 잉크를 제작하였으며, 노즐의 두께와 유량을 변화하여 패터닝 결과물을 제작하였고, 전도성 입자 잉크의 토출에 따른 전기전도도를 도출하였다.

• 한국산학기술학회논문지
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• 제16권10호
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• pp.6925-6931
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• 2015

LED(Light Emitting Diode)는 저 전력, 긴 수명, 고 휘도, 빠른 응답, 친환경적 특성으로 인해 조명, 디스플레이 등 여러 분야에 사용되고 있다. 백색광 발광다이오드 구현 방식에는 대표적으로 청색 LED 칩과 황색 형광체를 조합하여 백색광을 방출하는 유형이 사용 편리성, 경제성, 효율성 측면에서 LED 백라이트 유닛 및 LED 조명 제조에 가장 적합한 것으로 연구되어 실제 적용되고 있다. 백색광 구현 LED 칩 패키징 공정에서 청색 LED 칩에 황색 형광체에 실리콘을 혼합한 형광봉 지재를 토출하는 공정은 중요한 공정이다. 따라서 본 연구에서는 조명용 백색 LED 제조 공정에서 실리콘 봉지재를 토출하기 위하여 정전기력 방식과 보이스코일 모터를 이용하여 EHD 펌프 시스템을 개발하였다. 이를 위하여 인가전압 및 시간에 따른 유체곡면 형상을 확인하기 위하여 기초 토출 실험을 통해 최적의 토출 조건이 결정하였고 또한 검증을 위하여 실험계획법을 사용하였다. 검증된 토출 조건의 균일도를 확인하기 위하여 반복 토출 실험을 수행하였다.